Preliminary results from the High Speed Airframe Integration Research projectA review is presented of the accomplishment of the near term objectives of developing an analysis system and optimization methods during the first year of the NASA Langley High Speed Airframe Integration Research (HiSAIR) project. The characteristics of a Mach 3 HSCT transport have been analyzed utilizing the newly developed process. In addition to showing more detailed information about the aerodynamic and structural coupling for this type of vehicle, this exercise aided in further refining the data requirements for the analysis process.
Document ID
19920050572
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Coen, Peter G. (NASA Langley Research Center Hampton, VA, United States)
Sobieszczanski-Sobieski, Jaroslaw (NASA Langley Research Center Hampton, VA, United States)
Dollyhigh, Samuel M. (NASA Langley Research Center Hampton, VA, United States)